CN220884822U - Unmanned aerial vehicle's load equipment pendant - Google Patents
Unmanned aerial vehicle's load equipment pendant Download PDFInfo
- Publication number
- CN220884822U CN220884822U CN202322514206.3U CN202322514206U CN220884822U CN 220884822 U CN220884822 U CN 220884822U CN 202322514206 U CN202322514206 U CN 202322514206U CN 220884822 U CN220884822 U CN 220884822U
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- fixed
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- aerial vehicle
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- 238000013016 damping Methods 0.000 claims description 14
- 230000035939 shock Effects 0.000 claims description 8
- 230000000452 restraining effect Effects 0.000 claims 1
- 238000009434 installation Methods 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a load equipment pendant of an unmanned aerial vehicle, which comprises a fixed plate, wherein a fixed bin is fixed on one side of the fixed plate through bolts, a sliding rod is fixed in the fixed bin, and a fixed structure is arranged on the sliding rod; the fixed knot constructs including the fixed block, and the fixed block is fixed in the outside of slide bar, and the fixed block is provided with two sets of with respect to the vertical central line symmetry of slide bar, the bottom of fixed block is fixed with the sliding plate, and a plurality of spouts have been seted up to one side inner wall of sliding plate, the inside sliding connection of spout has the connecting rod, and one side of connecting rod is fixed with the movable plate, the one end of movable plate is fixed with the restriction piece, and the inside of restriction piece has been seted up first mounting hole to first mounting hole is provided with two sets of with respect to the vertical central line symmetry of restriction piece. The device to be fixed is placed at the bottom of the fixed bin, and the connecting rods are fixed on two sides of the moving plate.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a load equipment pendant of an unmanned aerial vehicle.
Background
With the development of unmanned aerial vehicle industry in recent years, the more popular the aerial photography and aerial mapping industries, the more popular the application of unmanned aerial vehicle or organic vehicle as aerial photography.
The utility model discloses a multipurpose unmanned aerial vehicle carrying hanging frame, which is disclosed as CN212290358U, and comprises a hanging frame, a hanging frame plate, a bolt and a nut, and is characterized in that: the hanging frame is connected with the left side and the right side above the hanging frame plate through bolts and nuts. The beneficial effects are that: the load hanging frame is free from disassembly, and one load hanging frame is used for carrying different special equipment, so that the universality is strong, the production cost is reduced, and the installation efficiency of the special equipment during replacement is improved.
In summary, the following technical problems exist in the prior art: the device is fixed through a plurality of mounting holes that set up of the left and right sides of the central line of hanging the frame board, but have the space around after fixing through bolt and nut, and the vibrations that produce in the flight offset easily, and for this reason, we provide a unmanned aerial vehicle's load equipment pendant.
Disclosure of utility model
The utility model aims to provide a load equipment pendant of an unmanned aerial vehicle so as to solve the problems in the background art.
In order to solve the technical problems, the utility model adopts the following technical scheme:
The load equipment pendant of the unmanned aerial vehicle comprises a fixed plate, wherein a fixed bin is fixed on one side of the fixed plate through bolts, a sliding rod is fixed in the fixed bin, and a fixed structure is arranged on the sliding rod;
The fixed knot constructs including the fixed block, and the fixed block is fixed in the outside of slide bar, and the fixed block is provided with two sets of with respect to the vertical central line symmetry of slide bar, the bottom of fixed block is fixed with the sliding plate, and a plurality of spouts have been seted up to one side inner wall of sliding plate, the inside sliding connection of spout has the connecting rod, and one side of connecting rod is fixed with the movable plate, the one end of movable plate is fixed with the restriction piece, and the inside of restriction piece has been seted up first mounting hole to the vertical central line symmetry of restriction piece is provided with two sets of, one side of fixed block is fixed with the handle, the movable plate is provided with two sets with respect to the vertical central line symmetry of sliding plate.
As still further aspects of the utility model: the center outside of slide bar is fixed with the baffle, the top of fixed storehouse is fixed with the lid through the bolt, and a plurality of second mounting holes have been seted up to the bottom inner wall of fixed storehouse.
As still further aspects of the utility model: the top of fixed plate is fixed with the connecting plate, and the fixed plate is provided with two sets of about the vertical central line symmetry of connecting plate.
As still further aspects of the utility model: the top of connecting plate is fixed with the installation pole through the bolt, and the top of installation pole is fixed with the restriction board.
As still further aspects of the utility model: the bottom of one end of the limiting plate is fixed with a spring, the bottom of the spring is fixed with a damping bin, the top of one end of the limiting plate is fixed with a damping ball, and the top of the damping ball is fixedly connected with the inner wall of the top of the damping bin.
As still further aspects of the utility model: the damping bin is symmetrically provided with two groups about the vertical center line of the limiting plate, and the limiting plate slides in the damping bin.
As still further aspects of the utility model: the top of shock attenuation storehouse is fixed with the backup pad, and the top of backup pad is fixed with the mounting panel to the mounting panel is provided with two sets of about the vertical central line symmetry of backup pad, and wherein the inside of mounting panel has seted up the third mounting hole.
The above description shows that the technical problems to be solved by the present application can be solved by the above technical solutions of the present application.
Meanwhile, through the technical scheme, the utility model has at least the following beneficial effects:
The utility model is provided with a fixing structure, devices to be fixed are placed at the bottom of a fixing bin, connecting rods are fixed at two sides of a moving plate, the moving plate is in sliding connection with a sliding groove formed in the sliding plate through the connecting rods, the moving plate is conveniently pulled by a handle, and a first mounting hole formed in a limiting block fixed on the moving plate is aligned with a mounting hole on the mounting device and is fixed through a bolt.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is a schematic diagram of a front cross-sectional structure of the present utility model;
FIG. 3 is a schematic perspective view of a mounting bar according to the present utility model;
FIG. 4 is a schematic view of a fastening structure according to the present utility model;
FIG. 5 is a schematic top view of a fixing structure according to the present utility model
Fig. 6 is a schematic perspective view of a fixing structure of the present utility model.
In the figure: 1. a fixing plate; 2. a fixed bin; 3. a slide bar; 4. a fixed structure; 401. a fixed block; 402. a sliding plate; 403. a chute; 404. a connecting rod; 405. a moving plate; 406. a limiting block; 407. a handle; 408. a first mounting hole; 5. a baffle; 6. a second mounting hole; 7. a cover; 8. a connecting plate; 9. a mounting rod; 10. a limiting plate; 11. a spring; 12. a damping bin; 13. a shock-absorbing ball; 14. a support plate; 15. a mounting plate; 16. and a third mounting hole.
Detailed Description
The present utility model will be described in further detail with reference to the drawings and examples, in order to make the objects, technical solutions and advantages of the present utility model more apparent. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the scope of the utility model.
Description of the preferred embodiments
As shown in fig. 1-3, the present utility model provides a technical solution: the utility model provides an unmanned aerial vehicle's load equipment pendant, including fixed plate 1, one side of fixed plate 1 is fixed with fixed bin 2 through the bolt, and the inside of fixed bin 2 is fixed with slide bar 3, and be provided with fixed knot structure 4 on the slide bar 3, the center outside of slide bar 3 is fixed with baffle 5, the top of fixed bin 2 is fixed with lid 7 through the bolt, and a plurality of second mounting holes 6 have been seted up to the bottom inner wall of fixed bin 2, the top of fixed plate 1 is fixed with connecting plate 8, and fixed plate 1 is provided with two sets of with respect to the vertical central line symmetry of connecting plate 8, the top of connecting plate 8 is fixed with mounting rod 9 through the bolt, and the top of mounting rod 9 is fixed with limiting plate 10, limiting plate 10's one end bottom is fixed with spring 11, and the bottom of spring 11 is fixed with shock attenuation storehouse 12, limiting plate 10's one end top is fixed with shock-absorbing ball 13, and the top inner wall fixed connection of shock attenuation storehouse 12, the vibrations that produce when unmanned aerial vehicle flies can cushion through spring 11 and shock attenuation ball 13, shock attenuation storehouse 12 limit for the vertical central line symmetry of 10 and limiting plate 10 are provided with two sets of limiting plate 10, and limiting plate 10 is provided with two sets of limiting plate 10 with vertical central line symmetry, and limiting plate 10's inside is fixed plate 14, limiting plate 15 is provided with the top 15 and is provided with the mounting plate 15 with the top 15, wherein the top 15 is fixed with the mounting plate 15.
Examples
The scheme in the first embodiment is further described below in conjunction with a specific working manner, and the details are described below:
As shown in fig. 4 to 6, as a preferred embodiment, further, the fixing structure 4 includes a fixing block 401, the fixing block 401 is fixed on the outer side of the sliding rod 3, two groups of fixing blocks 401 are symmetrically arranged on the bottom of the sliding rod 3 with respect to the vertical center line of the sliding rod 3, a sliding plate 402 is fixed on the bottom of the fixing block 401, a plurality of sliding grooves 403 are formed in one side inner wall of the sliding plate 402, a connecting rod 404 is slidably connected in the sliding groove 403, a moving plate 405 is fixed on one side of the connecting rod 404, a limiting block 406 is fixed on one end of the moving plate 405, a first mounting hole 408 is formed in the inside of the limiting block 406, two groups of first mounting holes 408 are symmetrically arranged on the vertical center line of the limiting block 406, a handle 407 is fixed on one side of the limiting block 406, a device to be fixed is placed on the bottom of the fixed bin 2, a connecting rod 404 is fixed on two sides of the moving plate 405, the moving plate 405 is slidably connected with the sliding grooves 403 formed in the sliding plate 402 through the connecting rod 404, the moving plate 405 is conveniently pulled through the handle 407, and the first mounting holes 408 formed in the limiting block 406 fixed on the moving plate 405 are aligned with the mounting holes through the mounting bolts.
From the above, it can be seen that:
the utility model aims at the technical problems that: the device is fixed through a plurality of mounting holes arranged on the left side and the right side of the center line of the hanging frame plate, but gaps are reserved in the front and the back after the device is fixed through bolts and nuts, so that vibration generated in flight is easy to deviate; the technical scheme of each embodiment is adopted. Meanwhile, the implementation process of the technical scheme is as follows:
Firstly, two ends of a limiting plate 10 are inserted into the inside of a damping bin 12 to be in contact with a spring 11 and a damping ball 13, an installation rod 9 is fixed at the bottom of the limiting plate 10, a connecting plate 8 is fixed at the bottom of the installation rod 9 through bolts, fixing plates 1 are fixed at two sides of the connecting plate 8, a fixing bin 2 is fixed between the fixing plates 1 through bolts, a sliding rod 3 is fixed in the inside of the fixing bin 2, and a fixing block 401 is fixed on the sliding rod 3;
Then, the device to be fixed is placed at the bottom of the fixed bin 2, connecting rods 404 are fixed at the two sides of a movable plate 405, the movable plate 405 is in sliding connection with a sliding groove 403 formed in the sliding plate 402 through the connecting rods 404, the movable plate 405 is conveniently pulled by a handle 407, a first mounting hole 408 formed in a limiting block 406 fixed on the movable plate 405 is aligned with a mounting hole on the mounting device, a bolt penetrates through the first mounting hole 408 and a second mounting hole 6 to fix the device, a cover 7 is fixed at the top of the fixed bin 2 through the bolt, and corrosion of internal parts caused by rainwater entering the fixed bin 2 when the unmanned aerial vehicle is used in rainy days can be prevented;
Finally, a supporting plate 14 is fixed on the top of the damping bin 12, a mounting plate 15 is fixed on the top of the supporting plate 14, and the device is fixed on the unmanned aerial vehicle through a third mounting hole 16 formed in the mounting plate 15.
Through the arrangement, the application can solve the technical problems, and simultaneously realize the following technical effects:
The utility model is provided with the fixed structure 4, a device to be fixed is placed at the bottom of the fixed bin 2, the two sides of the movable plate 405 are fixed with the connecting rods 404, the movable plate 405 is in sliding connection with the sliding grooves 403 arranged in the sliding plate 402 through the connecting rods 404, the movable plate 405 is conveniently pulled by the handles 407, the first mounting holes 408 arranged in the limiting blocks 406 fixed on the movable plate 405 are aligned with the mounting holes on the mounting device, and the fixing is carried out through bolts.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The unmanned aerial vehicle load equipment pendant is characterized by comprising a fixing plate (1), wherein a fixing bin (2) is fixed on one side of the fixing plate (1) through a bolt, a sliding rod (3) is fixed in the fixing bin (2), and a fixing structure (4) is arranged on the sliding rod (3);
Fixed knot constructs (4) including fixed block (401), fixed block (401) are fixed in the outside of slide bar (3), and fixed block (401) are provided with two sets of with respect to the vertical central line symmetry of slide bar (3), the bottom of fixed block (401) is fixed with sliding plate (402), and a plurality of spouts (403) have been seted up to one side inner wall of sliding plate (402), the inside sliding connection of spout (403) has connecting rod (404), and one side of connecting rod (404) is fixed with movable plate (405), one end of movable plate (405) is fixed with limiting block (406), and limiting block (406)'s inside has been seted up first mounting hole (408), and first mounting hole (408) are provided with two sets of with respect to the vertical central line symmetry of limiting block (406), one side of limiting block (406) is fixed with handle (407), movable plate (405) are provided with two sets with respect to the vertical central line symmetry of sliding plate (402).
2. The unmanned aerial vehicle load equipment pendant according to claim 1, wherein a baffle (5) is fixed on the outer side of the center of the sliding rod (3), a cover (7) is fixed on the top of the fixed bin (2) through bolts, and a plurality of second mounting holes (6) are formed in the inner wall of the bottom of the fixed bin (2).
3. The unmanned aerial vehicle load equipment pendant according to claim 1, wherein the top of the fixed plate (1) is fixed with a connecting plate (8), and the fixed plate (1) is symmetrically provided with two groups about the vertical center line of the connecting plate (8).
4. A load device pendant of an unmanned aerial vehicle according to claim 3, wherein the top of the connecting plate (8) is fixed with a mounting bar (9) by means of bolts, and the top of the mounting bar (9) is fixed with a restraining plate (10).
5. The unmanned aerial vehicle load equipment pendant according to claim 4, wherein a spring (11) is fixed at the bottom of one end of the limiting plate (10), a damping bin (12) is fixed at the bottom of the spring (11), a damping ball (13) is fixed at the top of one end of the limiting plate (10), and the top of the damping ball (13) is fixedly connected with the top inner wall of the damping bin (12).
6. The unmanned aerial vehicle load equipment pendant according to claim 5, wherein the shock absorbing bin (12) is symmetrically arranged with two groups about the vertical center line of the limiting plate (10), and the limiting plate (10) slides inside the shock absorbing bin (12).
7. The unmanned aerial vehicle load equipment pendant according to claim 6, wherein the top of the shock absorbing bin (12) is fixed with a supporting plate (14), the top of the supporting plate (14) is fixed with a mounting plate (15), and the mounting plate (15) is symmetrically provided with two groups about the vertical center line of the supporting plate (14), wherein a third mounting hole (16) is formed in the mounting plate (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322514206.3U CN220884822U (en) | 2023-09-15 | 2023-09-15 | Unmanned aerial vehicle's load equipment pendant |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322514206.3U CN220884822U (en) | 2023-09-15 | 2023-09-15 | Unmanned aerial vehicle's load equipment pendant |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220884822U true CN220884822U (en) | 2024-05-03 |
Family
ID=90839354
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322514206.3U Active CN220884822U (en) | 2023-09-15 | 2023-09-15 | Unmanned aerial vehicle's load equipment pendant |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220884822U (en) |
-
2023
- 2023-09-15 CN CN202322514206.3U patent/CN220884822U/en active Active
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